A Novel Fault Diagnosis Method Design and Application for Civil Aircraft System

被引:0
|
作者
Chen, Yongqi [1 ]
Zhong, Zhiguang [1 ]
机构
[1] Ningbo Univ, CST, Intelligence Sci & Electromech syst Lab, Ningbo 315211, Zhejiang, Peoples R China
关键词
Fault observer; support vector machines; compensation term; proportional multiple-integral observer; OBSERVER; SCHEME;
D O I
10.1109/ICAL.2009.5262684
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
For estimating faults of the system with unknown nonlinear term, a novel fault diagnosis method based on nonlinear compensation term and proportional multiple-integral observer is proposed. In this method, the nonlinear compensation term is constructed by support vector machines(SVM), which can reduce the influence of unknown nonlinear part. Proportional multiple-integral observer based nonlinear compensation term can estimate actuator faults when there are sensor faults or output disturbance in the system. The proposed method is applied in civil aircraft system. Simulation experiments are given to demonstrate the efficiency.
引用
收藏
页码:1643 / 1647
页数:5
相关论文
共 50 条
  • [21] Design of Fault Diagnosis Expert System for Certain Type of Aircraft Electrical Power
    Cao Jun-bin
    Guo Er-min
    Li Yan
    [J]. INTELLIGENT SYSTEM AND APPLIED MATERIAL, PTS 1 AND 2, 2012, 466-467 : 1186 - +
  • [22] A Novel Aircraft Fault Diagnosis and Prognosis System based on Gaussian Mixture Models
    Wang, ZeFeng
    Zarader, Jean-Luc
    Argentieri, Sylvain
    [J]. 2012 12TH INTERNATIONAL CONFERENCE ON CONTROL, AUTOMATION, ROBOTICS & VISION (ICARCV), 2012, : 1794 - 1799
  • [23] Fault Diagnosis Method for An Aircraft Attitude Control System based on Deep Learning
    Luo, Xiaoli
    Wang, Wei
    Hu, Hui
    Cheng, Zhongtao
    Tang, Maoqin
    Wang, Bo
    Liu, Lei
    [J]. PROCEEDINGS OF THE 33RD CHINESE CONTROL AND DECISION CONFERENCE (CCDC 2021), 2021, : 2078 - 2085
  • [24] A Forward Development Method for Functional Design of Civil Aircraft Flight Control System
    Cheng S.
    Li C.
    Zhang Y.
    Tang C.
    Meng X.
    Xie Y.
    [J]. Shanghai Jiaotong Daxue Xuebao/Journal of Shanghai Jiaotong University, 2023, 57 (10): : 1305 - 1315
  • [25] A Multivalued Test and Diagnostic Strategy Optimization Method for Aircraft System Fault Diagnosis
    Su, Yan
    Liang, Xuerui
    Gu, Chenxuan
    Khemani, Varun
    Pecht, Michael
    [J]. 2019 IEEE INTERNATIONAL CONFERENCE ON PROGNOSTICS AND HEALTH MANAGEMENT (ICPHM), 2019,
  • [26] Architecture design method for Structural Health Monitoring System(SHM) of Civil Aircraft
    Wei, Yuanlei
    Gao, Feipeng
    [J]. 2017 INTERNATIONAL CONFERENCE ON SENSING, DIAGNOSTICS, PROGNOSTICS, AND CONTROL (SDPC), 2017, : 736 - 739
  • [27] A Fault Diagnosis Framework for Aircraft Electromechanical System
    Liu, Haigang
    Sheng, Shouzhao
    [J]. PROCEEDINGS OF THE 2021 IEEE 16TH CONFERENCE ON INDUSTRIAL ELECTRONICS AND APPLICATIONS (ICIEA 2021), 2021, : 2014 - 2019
  • [28] Application of a Novel Adaptive Med Fault Diagnosis Method in Gearboxes
    Du, Wenhua
    Guo, Xiaoming
    Han, Xiaofeng
    Wang, Junyuan
    Zhou, Jie
    Wang, Zhijian
    Yao, Xingyan
    Shao, Yanjun
    Wang, Guanjun
    [J]. ENTROPY, 2019, 21 (11)
  • [29] Design of generalized fault diagnosis observer and active adaptive fault tolerant controller for aircraft control system
    Sun, Rong
    Han, Yuntao
    Wang, Yingying
    [J]. MATHEMATICAL BIOSCIENCES AND ENGINEERING, 2022, 19 (06) : 5591 - 5609
  • [30] Design and Application of a Reconstruction System for Engineering Equipment Fault Diagnosis
    LI Jie1
    2 Xuzhou Air Force College
    3 Command Institution of Engineering Corps
    [J]. International Journal of Plant Engineering and Management, 2009, 14 (03) : 136 - 141